Yaw and Pitch
There may well be an airframe reaction with some types but it is usually a propellor effect.
What is usually encounted is that the aircraft will pitch up when yawing right and down when yawing left (on engines that rotate to the right - such as Lycoming and TCM)
The thrust from a propellor is not symetrical. The down going blade produces greater thrust than the upgoing blade. This effect changes with angle of attack. Yaw to the right and the angle of attack of the down going blade increases. Increase thrust and the aircraft pitches up, decrease thrust and the aircraft pitches down. Torque must also be a consideration. A gyro will react 90 degrees to the force applied. Tail dragger pilots know that well!